View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58661U 26145.60325855 +.00000000 +00000-0 +25093-3 0 00003
2 58661 97.4417 262.4095 0008033 54.3943 305.8046 15.32363774 07
| Epoch (UTC): | 25 May 2026 14:28:41 |
| Eccentricity: | 0.0008033 |
| inclination: | 97.4417° |
| perigee height: | 463 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 262.4095° |
| argument of perigee: | 54.3943° |
| revolutions per day: | 15.32363774 |
| mean anomaly at epoch: | 305.8046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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